CN1552017B - Material and method for three-dimensional modeling - Google Patents
Material and method for three-dimensional modeling Download PDFInfo
- Publication number
- CN1552017B CN1552017B CN028096924A CN02809692A CN1552017B CN 1552017 B CN1552017 B CN 1552017B CN 028096924 A CN028096924 A CN 028096924A CN 02809692 A CN02809692 A CN 02809692A CN 1552017 B CN1552017 B CN 1552017B
- Authority
- CN
- China
- Prior art keywords
- thermoplastic resin
- resin
- ppsu
- potpourri
- modeling
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 239000000463 material Substances 0.000 title claims abstract description 202
- 238000000034 method Methods 0.000 title claims abstract description 37
- 229920000491 Polyphenylsulfone Polymers 0.000 claims abstract description 24
- 229920005992 thermoplastic resin Polymers 0.000 claims abstract description 23
- 229920006020 amorphous polyamide Polymers 0.000 claims abstract description 16
- 229920001955 polyphenylene ether Polymers 0.000 claims abstract description 13
- 229920002492 poly(sulfone) Polymers 0.000 claims abstract description 9
- 229920000098 polyolefin Polymers 0.000 claims abstract description 8
- 238000001125 extrusion Methods 0.000 claims description 41
- 229920005989 resin Polymers 0.000 claims description 29
- 239000011347 resin Substances 0.000 claims description 29
- 239000000155 melt Substances 0.000 claims description 14
- 239000004417 polycarbonate Substances 0.000 claims description 12
- 229920005668 polycarbonate resin Polymers 0.000 claims description 9
- 239000004431 polycarbonate resin Substances 0.000 claims description 9
- 238000010276 construction Methods 0.000 claims description 4
- 230000004927 fusion Effects 0.000 claims description 3
- 238000004519 manufacturing process Methods 0.000 claims description 3
- 238000009998 heat setting Methods 0.000 claims 4
- 239000012994 photoredox catalyst Substances 0.000 claims 2
- 239000011342 resin composition Substances 0.000 claims 2
- 239000000203 mixture Substances 0.000 abstract description 17
- 230000008021 deposition Effects 0.000 abstract description 5
- 239000012815 thermoplastic material Substances 0.000 abstract description 4
- 229920006258 high performance thermoplastic Polymers 0.000 abstract description 2
- 239000012778 molding material Substances 0.000 description 23
- 238000000465 moulding Methods 0.000 description 20
- 239000000945 filler Substances 0.000 description 14
- 229920000515 polycarbonate Polymers 0.000 description 9
- 239000004676 acrylonitrile butadiene styrene Substances 0.000 description 7
- 239000000654 additive Substances 0.000 description 7
- 238000000151 deposition Methods 0.000 description 7
- 230000009477 glass transition Effects 0.000 description 7
- 229920000642 polymer Polymers 0.000 description 7
- XECAHXYUAAWDEL-UHFFFAOYSA-N acrylonitrile butadiene styrene Chemical compound C=CC=C.C=CC#N.C=CC1=CC=CC=C1 XECAHXYUAAWDEL-UHFFFAOYSA-N 0.000 description 6
- 229920000122 acrylonitrile butadiene styrene Polymers 0.000 description 6
- 239000007787 solid Substances 0.000 description 6
- 238000011960 computer-aided design Methods 0.000 description 5
- 239000002994 raw material Substances 0.000 description 5
- 229910021536 Zeolite Inorganic materials 0.000 description 4
- 229920006125 amorphous polymer Polymers 0.000 description 4
- HNPSIPDUKPIQMN-UHFFFAOYSA-N dioxosilane;oxo(oxoalumanyloxy)alumane Chemical compound O=[Si]=O.O=[Al]O[Al]=O HNPSIPDUKPIQMN-UHFFFAOYSA-N 0.000 description 4
- 229920005669 high impact polystyrene Polymers 0.000 description 4
- 239000007788 liquid Substances 0.000 description 4
- 229920003023 plastic Polymers 0.000 description 4
- 239000004033 plastic Substances 0.000 description 4
- 239000000126 substance Substances 0.000 description 4
- 239000010457 zeolite Substances 0.000 description 4
- 230000000996 additive effect Effects 0.000 description 3
- 239000011324 bead Substances 0.000 description 3
- 239000002274 desiccant Substances 0.000 description 3
- 238000001035 drying Methods 0.000 description 3
- 229920003247 engineering thermoplastic Polymers 0.000 description 3
- 239000004797 high-impact polystyrene Substances 0.000 description 3
- 239000008188 pellet Substances 0.000 description 3
- 230000008569 process Effects 0.000 description 3
- 238000007711 solidification Methods 0.000 description 3
- 230000008023 solidification Effects 0.000 description 3
- 238000012360 testing method Methods 0.000 description 3
- 229920001169 thermoplastic Polymers 0.000 description 3
- 239000004416 thermosoftening plastic Substances 0.000 description 3
- VTYYLEPIZMXCLO-UHFFFAOYSA-L Calcium carbonate Chemical compound [Ca+2].[O-]C([O-])=O VTYYLEPIZMXCLO-UHFFFAOYSA-L 0.000 description 2
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 2
- 230000008859 change Effects 0.000 description 2
- 230000007423 decrease Effects 0.000 description 2
- 238000013461 design Methods 0.000 description 2
- 230000009969 flowable effect Effects 0.000 description 2
- 238000013007 heat curing Methods 0.000 description 2
- 239000002808 molecular sieve Substances 0.000 description 2
- -1 polyaryletherkotone Polymers 0.000 description 2
- 238000000518 rheometry Methods 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- ODINCKMPIJJUCX-UHFFFAOYSA-N Calcium oxide Chemical compound [Ca]=O ODINCKMPIJJUCX-UHFFFAOYSA-N 0.000 description 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 229920000049 Carbon (fiber) Polymers 0.000 description 1
- 239000004793 Polystyrene Substances 0.000 description 1
- 239000000853 adhesive Substances 0.000 description 1
- 230000001070 adhesive effect Effects 0.000 description 1
- HZVVJJIYJKGMFL-UHFFFAOYSA-N almasilate Chemical compound O.[Mg+2].[Al+3].[Al+3].O[Si](O)=O.O[Si](O)=O HZVVJJIYJKGMFL-UHFFFAOYSA-N 0.000 description 1
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 1
- 238000004873 anchoring Methods 0.000 description 1
- 239000003963 antioxidant agent Substances 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 229910000019 calcium carbonate Inorganic materials 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 239000006229 carbon black Substances 0.000 description 1
- 239000004917 carbon fiber Substances 0.000 description 1
- 230000015556 catabolic process Effects 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 238000007796 conventional method Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 238000001723 curing Methods 0.000 description 1
- 238000006731 degradation reaction Methods 0.000 description 1
- 230000000593 degrading effect Effects 0.000 description 1
- 239000000975 dye Substances 0.000 description 1
- 238000005265 energy consumption Methods 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 239000003365 glass fiber Substances 0.000 description 1
- 239000008187 granular material Substances 0.000 description 1
- 229910002804 graphite Inorganic materials 0.000 description 1
- 239000010439 graphite Substances 0.000 description 1
- 230000020169 heat generation Effects 0.000 description 1
- 239000012761 high-performance material Substances 0.000 description 1
- 230000001771 impaired effect Effects 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000010030 laminating Methods 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 239000010445 mica Substances 0.000 description 1
- 229910052618 mica group Inorganic materials 0.000 description 1
- 239000004005 microsphere Substances 0.000 description 1
- 239000012768 molten material Substances 0.000 description 1
- 230000000704 physical effect Effects 0.000 description 1
- 239000000049 pigment Substances 0.000 description 1
- 239000004014 plasticizer Substances 0.000 description 1
- 229920003229 poly(methyl methacrylate) Polymers 0.000 description 1
- 239000002861 polymer material Substances 0.000 description 1
- 239000004926 polymethyl methacrylate Substances 0.000 description 1
- 229920002223 polystyrene Polymers 0.000 description 1
- 150000003839 salts Chemical class 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 229910010271 silicon carbide Inorganic materials 0.000 description 1
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 1
- 239000000377 silicon dioxide Substances 0.000 description 1
- 239000000779 smoke Substances 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- 230000001954 sterilising effect Effects 0.000 description 1
- 238000004659 sterilization and disinfection Methods 0.000 description 1
- 239000000454 talc Substances 0.000 description 1
- 229910052623 talc Inorganic materials 0.000 description 1
- 229910052882 wollastonite Inorganic materials 0.000 description 1
- 239000010456 wollastonite Substances 0.000 description 1
Images
Classifications
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08K—Use of inorganic or non-macromolecular organic substances as compounding ingredients
- C08K5/00—Use of organic ingredients
- C08K5/0008—Organic ingredients according to more than one of the "one dot" groups of C08K5/01 - C08K5/59
- C08K5/0016—Plasticisers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C33/00—Moulds or cores; Details thereof or accessories therefor
- B29C33/38—Moulds or cores; Details thereof or accessories therefor characterised by the material or the manufacturing process
- B29C33/40—Plastics, e.g. foam or rubber
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C41/00—Shaping by coating a mould, core or other substrate, i.e. by depositing material and stripping-off the shaped article; Apparatus therefor
- B29C41/34—Component parts, details or accessories; Auxiliary operations
- B29C41/36—Feeding the material on to the mould, core or other substrate
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C64/00—Additive manufacturing, i.e. manufacturing of three-dimensional [3D] objects by additive deposition, additive agglomeration or additive layering, e.g. by 3D printing, stereolithography or selective laser sintering
- B29C64/10—Processes of additive manufacturing
- B29C64/106—Processes of additive manufacturing using only liquids or viscous materials, e.g. depositing a continuous bead of viscous material
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C64/00—Additive manufacturing, i.e. manufacturing of three-dimensional [3D] objects by additive deposition, additive agglomeration or additive layering, e.g. by 3D printing, stereolithography or selective laser sintering
- B29C64/10—Processes of additive manufacturing
- B29C64/106—Processes of additive manufacturing using only liquids or viscous materials, e.g. depositing a continuous bead of viscous material
- B29C64/118—Processes of additive manufacturing using only liquids or viscous materials, e.g. depositing a continuous bead of viscous material using filamentary material being melted, e.g. fused deposition modelling [FDM]
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C64/00—Additive manufacturing, i.e. manufacturing of three-dimensional [3D] objects by additive deposition, additive agglomeration or additive layering, e.g. by 3D printing, stereolithography or selective laser sintering
- B29C64/40—Structures for supporting 3D objects during manufacture and intended to be sacrificed after completion thereof
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B33—ADDITIVE MANUFACTURING TECHNOLOGY
- B33Y—ADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3-D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3-D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
- B33Y10/00—Processes of additive manufacturing
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B33—ADDITIVE MANUFACTURING TECHNOLOGY
- B33Y—ADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3-D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3-D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
- B33Y70/00—Materials specially adapted for additive manufacturing
- B33Y70/10—Composites of different types of material, e.g. mixtures of ceramics and polymers or mixtures of metals and biomaterials
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C71/00—After-treatment of articles without altering their shape; Apparatus therefor
- B29C71/02—Thermal after-treatment
- B29C2071/022—Annealing
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C2791/00—Shaping characteristics in general
- B29C2791/004—Shaping under special conditions
- B29C2791/005—Using a particular environment, e.g. sterile fluids other than air
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C41/00—Shaping by coating a mould, core or other substrate, i.e. by depositing material and stripping-off the shaped article; Apparatus therefor
- B29C41/34—Component parts, details or accessories; Auxiliary operations
- B29C41/52—Measuring, controlling or regulating
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C71/00—After-treatment of articles without altering their shape; Apparatus therefor
- B29C71/02—Thermal after-treatment
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2055/00—Use of specific polymers obtained by polymerisation reactions only involving carbon-to-carbon unsaturated bonds, not provided for in a single one of main groups B29K2023/00 - B29K2049/00, e.g. having a vinyl group, as moulding material
- B29K2055/02—ABS polymers, i.e. acrylonitrile-butadiene-styrene polymers
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B2219/00—Program-control systems
- G05B2219/30—Nc systems
- G05B2219/49—Nc machine tool, till multiple
- G05B2219/49019—Machine 3-D slices, to build 3-D model, stratified object manufacturing SOM
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Optics & Photonics (AREA)
- Ceramic Engineering (AREA)
- Civil Engineering (AREA)
- Composite Materials (AREA)
- Structural Engineering (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Medicinal Chemistry (AREA)
- Polymers & Plastics (AREA)
- Organic Chemistry (AREA)
- Health & Medical Sciences (AREA)
- Compositions Of Macromolecular Compounds (AREA)
Abstract
Description
技术领域technical field
本发明涉及使用加成法造型技术(additive process modelingtechniques)的三维物体的生产。更特别地,本发明涉及以预定图案堆积第一种可固化材料形成三维物体,同时堆积第二种可固化材料为正建造的三维物体提供支撑结构。The present invention relates to the production of three-dimensional objects using additive process modeling techniques. More particularly, the invention relates to depositing a first curable material in a predetermined pattern to form a three-dimensional object while depositing a second curable material to provide a support structure for the three-dimensional object being built.
背景技术Background technique
加成法造型机器根据计算机辅助设计(CAD)系统提供的设计数据积累造型介质制成三维模型。三维模型被用来提供包括审美判断、检验数学CAD模型、形成硬加工(forming hard tooling)、研究干扰和空间分配以及试验功能的功能。一种技术是根据CAD系统提供的设计数据以预定图案堆积可固化造型材料,多层累积形成模型。The additive method modeling machine makes a three-dimensional model according to the design data provided by the computer-aided design (CAD) system and accumulates the modeling medium. The 3D model is used to provide functions including aesthetic judgment, inspection of mathematical CAD models, forming hard tooling, study of interference and space allocation, and testing of functions. One technique is to pile up curable modeling materials in a predetermined pattern according to the design data provided by the CAD system, and accumulate multiple layers to form a model.
转让给本发明的受让人即Stratasys公司的Valavaara的美国专利4,749,347号、Crump的美国专利5,121,329号、Batchelder等人的美国专利5,303,141号、Crump的美国专利5,340,433号、Batchelder等人的美国专利5,402,351号、Crump等人的美国专利5,503,785号、Batchelder等人的美国专利5,764,521号、Danforth等人的美国专利5,900,207号、Batchelder等人的美国专利5,968,561号和Stuffle等人的美国专利6,067,480号描述了堆积多层从挤出头出来的可固化造型材料制成三维模型的设备和方法的实例。造型材料可以固体形式供应给挤出头,例如以缠在供应轴上的柔韧细丝形式或以固体棒的形式,如美国专利5,121,329号所公开的那样。如美国专利4,749,347号描述的,造型材料也可以以液体形式从存储器中抽出。在任何情况下,挤出头从一个喷嘴挤出熔融的造型材料到底部上。挤出的材料在CAD模型定义的区域上一层一层地堆积。被用作造型材料的可固化材料在固化时以足够的粘合力粘附在前面一层。发现热塑性材料特别适合这些堆积造型技术。U.S. Patent No. 4,749,347 to Valavaara, U.S. Patent No. 5,121,329 to Crump, U.S. Patent No. 5,303,141 to Batchelder et al., U.S. Patent No. 5,340,433 to Crump, U.S. Patent No. 5,402,351 to Batchelder et al. , U.S. Patent No. 5,503,785 to Crump et al., U.S. Patent No. 5,764,521 to Batchelder et al., U.S. Patent No. 5,900,207 to Danforth et al., U.S. Patent No. 5,968,561 to Batchelder et al., and U.S. Patent No. 6,067,480 to Stuffle et al. Example of an apparatus and method for forming a three-dimensional model from a curable modeling material exiting an extrusion head. The molding material may be supplied to the extrusion head in solid form, for example in the form of a flexible filament wound on a supply shaft or in the form of a solid rod as disclosed in US Pat. No. 5,121,329. The modeling material may also be withdrawn from the reservoir in liquid form as described in US Patent No. 4,749,347. In any case, the extrusion head extrudes molten molding material from a nozzle onto the base. The extruded material is built up layer by layer over the area defined by the CAD model. The curable material used as the modeling material adheres to the previous layer with sufficient adhesive force when cured. Thermoplastic materials were found to be particularly suitable for these build-up molding techniques.
用加成法技术创造三维物体时,例如堆积多层可固化材料,无一例外地,必须在造型材料本身不能直接支撑的建造中的建筑物体的突出部分下面或洞里使用支撑层或结构。例如,如果物体是一个地下空洞内部的模型,空洞的原型是从地层到天花板进行建筑的,这时钟乳石状物将需要一个临时支撑物直到天花板完成。同样因其它原因也需要支撑层或结构,例如把模型从底部移出,抵抗部分完成时模型的变形趋势,抵抗建筑过程施加给部分完成的模型的力量。When creating three-dimensional objects using additive techniques, such as stacking multiple layers of curable materials, it is invariably necessary to use support layers or structures under protrusions or in cavities of building objects under construction that cannot be directly supported by the modeling material itself. For example, if the object is a model of the interior of an underground cavity, the prototype of which is built from the ground floor to the ceiling, the stalactite will require a temporary support until the ceiling is complete. A support layer or structure is also needed for other reasons, such as to move the model out of the base, to resist the tendency of the model to deform when it is partially completed, and to resist the forces imposed on the partially completed model by the building process.
支撑结构可以使用堆积造型材料的相同堆积技术和设备建成。设备在合适的软件控制下为用作正形成的物体的悬空或自由空间部分的支撑结构生产附加几何形状。支撑材料或者从造型设备内的一个独立分配头堆积,或者用堆积造型材料的同一分配头堆积。选择支撑材料使其能粘合在造型材料上。将模型锚定在这样的支撑结构上解决了建造模型的问题,但是产生了另外的问题,即如何在不损坏模型的情况下从完成的模型中移开支撑结构。Support structures can be built using the same build-up techniques and equipment used to build up molding materials. The apparatus, under suitable software control, produces additional geometries for the support structures that serve as suspended or free-space portions of the object being formed. The support material is either deposited from a separate dispensing head within the molding apparatus or from the same dispensing head that deposits the molding material. The support material is selected so that it can be bonded to the modeling material. Anchoring the model to such a support structure solves the problem of building the model, but creates the additional problem of how to remove the support structure from the finished model without damaging the model.
除去支撑结构的问题已通过在模型和支撑结构之间形成弱的易碎结合解决,例如美国专利5,503,785号描述的。5,503,785号专利公开了一种方法,选择能和造型材料形成弱的易碎结合的材料作为支撑或脱离材料。支撑材料堆积在物体及其支撑结构的界面,或以层状方式堆积形成支撑结构,无论哪种情况,在物体成型后都使支撑结构脱离开。The problem of removing the support structure has been solved by creating a weak, fragile bond between the model and the support structure, such as described in US Patent No. 5,503,785. The 5,503,785 patent discloses a method of selecting a support or release material that forms a weak, brittle bond with the molding material. The support material builds up at the interface of the object and its support structure, or builds up in a layered fashion to form the support structure, in either case allowing the support structure to detach after the object has been formed.
现有技术中三维造型机使用丙烯腈-丁二烯-苯乙烯(ABS)热塑组分或蜡材料作造型材料。用作支撑材料的材料是高冲击聚苯乙烯。现有技术的细丝供料的三维造型机中,造型材料(或支撑材料)的细丝束由发动机驱动的一对供料轴推动前进进入挤出头携带的液化器。在液化器里,细丝被加热到一个可流动温度。供料轴将细丝束泵入液化器而使液化器加压。细丝束本身起活塞作用,形成一个泵。当供料轴继续推动细丝进入挤出头,进来的细丝束的力量将可流动材料从分配喷嘴挤出来,在分配喷嘴上堆积在可移到建筑平台上的底板上。in the prior art Three-dimensional modeling machines use acrylonitrile-butadiene-styrene (ABS) thermoplastic components or wax materials as modeling materials. The material used as support material is high impact polystyrene. prior art filament feed In the three-dimensional molding machine, the filament bundle of the modeling material (or supporting material) is pushed forward by a pair of feeding shafts driven by the engine and enters the liquefier carried by the extrusion head. In the liquefier, the filament is heated to a flowable temperature. The feed shaft pumps the filament tow into the liquefier to pressurize the liquefier. The filament bundle itself acts as a piston, forming a pump. As the feed shaft continues to push the filament into the extrusion head, the force of the incoming filament bundle extrudes the flowable material out of the dispensing nozzle where it deposits on a base plate that can be moved onto the building platform.
美国专利6,067,480号公开了一种分层堆积高强度工程聚合物加工耐用的三维物体的设备和方法。聚合物的原料棒用放置在缸内的活塞从挤出缸里挤出,提供低熔体流动和长链长的聚合物的高压挤出供应。6,067,480号公开,聚碳酸酯、聚芳基醚酮(polyaryletherkotone)和聚甲基丙烯酸甲酯的原料棒用挤出缸设备成功地挤出。6,067,480号专利没有公开支撑材料。US Patent No. 6,067,480 discloses an apparatus and method for layering high-strength engineering polymers to fabricate durable three-dimensional objects. A raw rod of polymer is extruded from an extrusion cylinder with a piston placed inside the cylinder, providing a high pressure extrusion supply of low melt flow and long chain length polymers. No. 6,067,480 discloses that rods of polycarbonate, polyaryletherkotone, and polymethylmethacrylate were successfully extruded using extrusion cylinder equipment. The 6,067,480 patent does not disclose support materials.
分层堆积高强度的工程热塑性塑料的设备和方法在PCT申请US00/17363号中公开。‘363号申请公开了用高温热塑性塑料建造模型。没有教导支撑材料。Apparatus and methods for layering high strength engineering thermoplastics are disclosed in PCT Application No. US00/17363. The '363 application discloses building models from high temperature thermoplastics. Support material is not taught.
仍然需要用高性能工程热塑性塑料建造模型,改进模型强度和质量。需要和造型方法相适应的材料为这些高性能材料建造成的模型提供合适的支撑结构。There remains a need to construct models with high performance engineering thermoplastics to improve model strength and quality. Materials compatible with the modeling method are required to provide suitable support structures for models built from these high-performance materials.
发明内容Contents of the invention
本发明是用于用熔融堆积造型技术(fused deposition modelingtechniques)建造模型及其支撑物的高性能热塑性材料。热挠曲温度(heatdeflection temperature)高于120℃的无定形热塑性树脂组成造型材料。在优选方案中,组成造型材料的热塑性树脂选自聚碳酸酯树脂、聚苯砜树脂和聚碳酸酯/丙烯腈-丁二烯-苯乙烯树脂组成的组中。自层合(self-laminate)的无定形热塑性树脂和造型材料粘合较弱,具有类似于造型材料的热挠曲温度的热挠曲温度,抗张强度在34MPa(5000psi)和83MPa(12000psi)之间,该材料包括支撑材料。在优选方案中,组成支撑材料的热塑性树脂选自聚亚苯基醚和聚烯烃的混合物、聚苯砜和无定形聚酰胺的混合物、聚苯砜和聚砜以及无定形聚酰胺的混合物组成的组中。The present invention is a high-performance thermoplastic material for building models and their supports using fused deposition modeling techniques. An amorphous thermoplastic resin with a heat deflection temperature higher than 120° C. constitutes the molding material. In a preferred embodiment, the thermoplastic resin constituting the modeling material is selected from the group consisting of polycarbonate resin, polyphenylsulfone resin and polycarbonate/acrylonitrile-butadiene-styrene resin. The self-laminated amorphous thermoplastic resin and the modeling material are weakly bonded, have a heat deflection temperature similar to that of the modeling material, and have a tensile strength of 34MPa (5000psi) and 83MPa (12000psi) In between, the material includes support material. In a preferred embodiment, the thermoplastic resin constituting the support material is selected from a mixture of polyphenylene ether and polyolefin, a mixture of polyphenylsulfone and amorphous polyamide, a mixture of polyphenylsulfone and polysulfone, and amorphous polyamide. group.
附图简要说明Brief description of the drawings
图1是表示用分层挤出技术形成的模型及其支撑结构的图形说明。Figure 1 is a graphical illustration showing a model and its supporting structure formed by layered extrusion techniques.
具体实施方式Detailed ways
参照图1所示类型的堆积造型系统描述本发明。图1表示建造本发明的支撑结构28支撑的模型26的挤出设备10。挤出设备10包括挤出头12、材料接收底部14和材料供应18。相对于以垂直的Z方向移动的底部14,挤出头12以X和Y方向移动。材料供应18给挤出头12供应材料的原料。在描述的方案中,材料的固体原料供应给挤出头12,在挤出头12携带的液化器22中熔融。液化器22加热原材料至稍高于其固化点的温度,使其还原为熔融状态。熔融材料通过液化器22的喷嘴24挤出到底部14上。原料可以是连续的细丝、棒、块、球、粒等形式。The invention is described with reference to a build-up molding system of the type shown in FIG. 1 . Figure 1 shows an
控制挤出头的移动将材料以多种路径和层堆积在底部14上建造三维模型26,进一步建造支撑结构28,限定支撑结构28以实质支撑正建造的模型26。在环境能控制的促进热固化的建造膛(未表示出)里在底部14上建成模型26及其支撑结构28。堆积材料的第一层粘附在底部14上形成地基,以后的每层材料相互粘结。Controlling the movement of the extrusion head builds up the material in various paths and layers onto the base 14 to build the three-
分配造型材料A形成模型26,相应于分配造型材料A,分配支撑材料B形成支撑结构28。为了方便,挤出设备10仅表示出一个材料供应18。但是应该理解,在本发明的实施中,造型材料A和支撑材料B从各自的材料供应供应给挤出设备10以各自的原材料。挤出设备10可以适应两种不同材料的分配:(1)配置两个挤出头12,一个供应有造型材料A,一个供应有支撑材料B(例如Batchelder的‘561专利公开的);(2)配置单一挤出头,所述单一挤出头供应有造型材料A和支撑材料B,用单一喷嘴分配两种材料(例如Crump的‘329专利的图6所示);或(3)配置单一挤出头供应两种材料,每种材料用各自的喷嘴分配(例如Crump的‘785专利的图6所示)Modeling material A is dispensed to form the
在描述的方案中,造型材料A和支撑材料B从挤出头出来以水平层状按实质上连续的路径堆积,以固体形式供应给挤出头。本领域熟练的人员可以理解本发明能有利地用多种其它型号的造型机实施,材料也可以以液体形式供应给挤出头。In the described solution, the molding material A and the support material B emerge from the extrusion head in horizontal layers in a substantially continuous path and are supplied in solid form to the extrusion head. Those skilled in the art will understand that the invention can be advantageously practiced with various other types of molding machines, and that the material can also be supplied to the extrusion head in liquid form.
本发明提供玻璃化转变温度高于120℃、从液体转变为固体时没有明显收缩的高性能工程热塑性树脂作为造型材料A。优选的热塑性树脂选自聚碳酸酯树脂、聚碳酸酯/丙烯腈-丁二烯-苯乙烯树脂和聚苯砜树脂组成的组中。本发明的支撑材料B是耐热性和收缩性类似于造型材料A、并且较弱地层合到模型上使其能在材料界面脱离的自层合热塑性树脂。另外,支撑材料B足够强以支撑模型。本发明的热塑性材料和目前用于熔融堆积造型的材料相比具有更高的冲击强度、更大的刚性、更高的热挠曲温度和更高的化学稳定性。如本领域熟练人员意识到的,本发明的造型和支撑材料可以包括填充物和其它添加剂,可提高热塑性树脂的其它性质。The present invention provides a high-performance engineering thermoplastic resin with a glass transition temperature higher than 120°C and no obvious shrinkage when changing from a liquid to a solid as the molding material A. Preferred thermoplastic resins are selected from the group consisting of polycarbonate resins, polycarbonate/acrylonitrile-butadiene-styrene resins and polyphenylsulfone resins. The support material B of the present invention is a self-laminating thermoplastic resin similar in heat resistance and shrinkage to the modeling material A, and weakly laminated to the mold so that it can be detached at the material interface. Additionally, support material B is strong enough to support the model. The thermoplastic material of the present invention has higher impact strength, greater rigidity, higher heat deflection temperature and higher chemical stability than materials currently used for fusion deposition molding. As will be appreciated by those skilled in the art, the build and support materials of the present invention may include fillers and other additives that may enhance other properties of the thermoplastic resin.
造型和支撑材料的流变学Rheology of molding and support materials
造型材料A和支撑材料B必须满足使用它们的特殊造型系统的大量造型标准,一般涉及热性质、强度、粘度和粘着力。Build material A and support material B must meet a number of build criteria for the particular build system in which they are used, generally relating to thermal properties, strength, viscosity and adhesion.
造型材料A和支撑材料B必须具有适合于造型过程的熔融粘度。理想地,用于熔融堆积造型的材料具有低的熔融粘度。熔融粘度在挤出温度必须足够低,使其总体上以连续的条道(road)或珠挤出。而且挤出温度下的熔融粘度必须足够低使材料的堆积的条道或珠几乎没有熔融强度,使其平展开,而不是卷起。增加挤出材料时的温度降低熔融粘度。但是挤出温度太高会引起受热的材料在挤出机里无用而分解。如果分解,在没有正切割装置(positive cut-off mechanism)的抽丝挤压机的情况下,材料将无法控制地从液化器排出进入建造袋里,出现一种称为“软泥”的情形。而且低的挤出温度减少能量消耗,减少热量产生和减少降解聚合物材料的几率。Modeling material A and support material B must have a melt viscosity suitable for the molding process. Ideally, the material used in melt deposition modeling has a low melt viscosity. The melt viscosity must be low enough at the extrusion temperature that it generally extrudes in a continuous road or bead. Also, the melt viscosity at extrusion temperatures must be low enough that the packed strands or beads of material have little melt strength, causing them to spread out rather than roll up. Increasing the temperature at which the material is extruded decreases the melt viscosity. But extrusion temperatures that are too high can cause the heated material to decompose uselessly in the extruder. If disintegrated, in the absence of a positive cut-off mechanism, the material will drain uncontrollably from the liquefier into the build bag, a condition known as "slime" . Moreover, the low extrusion temperature reduces energy consumption, reduces heat generation and reduces the chance of degrading polymer materials.
在理论上,熔融体的粘度和材料的分子量有关,当它接近临界分子量时,性质消失。因此熔融粘度的低限值定义为临界分子量的粘度,但是实际上所有的商业级聚合物超过临界分子量表现出良好的物理性质。In theory, the viscosity of the melt is related to the molecular weight of the material, and when it approaches the critical molecular weight, the properties disappear. The lower limit of melt viscosity is therefore defined as the critical molecular weight viscosity, but practically all commercial grade polymers exhibit good physical properties above the critical molecular weight.
熔融粘度用其相反的参数熔体流动测定。在带抽丝挤压机的 造型机中制造模型使用的材料在挤出温度下必须具有高的熔体流动,以便于在相当低的压力约21MPa(3000psi)或以下以连续的珠挤出。抽丝型挤压机堆积的材料需要的高熔体流动大于约5gms/10min,在挤出温度和1.2kg的负荷下用ASTM D1238测定。最优选地,熔体流动在5-30g/10min之间。较低的熔体流动(高粘度)适合高压挤出,例如用美国专利6,067,480号公开的设备。Melt viscosity is measured by its inverse parameter, melt flow. with wire extruder The material used to make the model in the molding machine must have high melt flow at the extrusion temperature in order to facilitate continuous bead extrusion at a relatively low pressure of about 21MPa (3000psi) or below. Drawn-type extruder-packed material requires a high melt flow of greater than about 5 gms/10 min, as determined by ASTM D1238 at extrusion temperature and a load of 1.2 kg. Most preferably, the melt flow is between 5-30 g/10 min. Lower melt flow (high viscosity) is suitable for high pressure extrusion, such as with the equipment disclosed in US Patent No. 6,067,480.
为了适当地支撑建造中的模型,支撑材料B必须自身粘合(自层合)。支撑材料B必须和造型材料A(共碾压)形成弱的易分开的粘合,使其能不伤害模型地和完成的模型分离开。当支撑结构从底部建起时,支撑材料B必须另外和底部粘合。In order to properly support the model under construction, support material B must bond to itself (self-laminate). Support material B must form a weak, breakable bond with modeling material A (co-laminated) so that it can be separated from the finished model without damaging the model. When the support structure is built from the bottom, the support material B must additionally be bonded to the bottom.
为了生产尺寸精确的模型,造型和支撑材料必须在建造袋的条件下冷却时几乎没有收缩。支撑材料B的任何收缩必须匹配造型材料A。材料的收缩差别将沿模型/支撑结构接合点引起应力和粘合失败。根据ASTM喷射造型试验标准,无定形聚合物固化时典型地具有低于或等于0.01cm/cm(0.010inch/inch)的收缩。对于堆积造型目的无定形聚合物的收缩特性是可以接受的,然而结晶聚合物对于堆积造型来说收缩太高。可以向材料中添加填充物减小收缩。可以向本发明的材料中添加晶体添加剂,只要以足够小的量添加使得材料继续具有无定形聚合物的收缩特性。In order to produce dimensionally accurate models, the molding and support materials must show little shrinkage when cooled under the conditions in which the bag is built. Any shrinkage of support material B must match build material A. Differential shrinkage of the material will cause stress and bond failure along the model/support structure junction. Amorphous polymers typically have a shrinkage of less than or equal to 0.01 cm/cm (0.010 inch/inch) when cured according to the ASTM spray molding test standard. The shrinkage characteristics of amorphous polymers are acceptable for build-up purposes, however, the shrinkage of crystalline polymers is too high for build-up. Fillers can be added to the material to reduce shrinkage. Crystalline additives may be added to the materials of the present invention as long as they are added in small enough amounts that the material continues to have the shrinkage characteristics of an amorphous polymer.
根据完成模型的特殊应用可以选择特殊的造型材料A。支撑材料B必须在固体形式时具有足够的机械强度以便在模型的制造中支撑模型。支撑材料B必须抵抗造型材料A的力量,否则模型将有不需要的卷缩和变形。Special molding material A can be selected according to the special application of the finished model. The support material B must have sufficient mechanical strength in solid form to support the model during its manufacture. Support material B must resist the forces of modeling material A, otherwise the model will have unwanted curling and deformation.
造型材料A和支撑材料B,当以细丝或棒状形式供应时,必须足够强使其能无破裂地运输。当以细丝形式供应时,材料还必须具有能形成细丝、缠绕和解绕以及经挤出设备无破裂地供应的强度和挠性。类似地,以细丝形式供应的材料必须具有足够的刚性,经挤出设备供应时不被压缩力产生变形。Modeling material A and support material B, when supplied in filament or rod form, must be strong enough to be transported without breaking. When supplied in filament form, the material must also have the strength and flexibility to form filaments, wind and unwind, and supply through extrusion equipment without breakage. Similarly, materials supplied in filament form must be rigid enough not to be deformed by compressive forces when supplied through extrusion equipment.
至于热性质,造型材料A和支撑材料B应该具有类似的热挠曲性质,使得两种材料能成功地挤出到同一建造膛中。如美国专利5,866,058号叙述的,在一个温度加热到高于热塑性或其它可热固化的造型材料的固化温度的膛里建造模型,接着逐渐冷却,释放出材料的应力。应力从正建造的模型中释放出使得完成的模型无应力、几乎无变形。如‘058号专利进一步叙述的,造型材料应该具有高于建造膛温度的玻璃化转变温度(Tg),使得模型不会太软而下垂。因此建造膛的优选温度在造型材料A的固化温度和其蠕变松弛温度(蠕变松弛温度定义为应力松弛模数从其低温度限值降低10倍的点)之间的范围内。同样地,支撑材料B的玻璃化转变温度应该高于建造膛的温度,这样,支撑结构不变形,维持其支撑的模型的结构逼真性。经过试验发现支撑材料B的玻璃化转变温度(或热挠曲温度)应该在造型材料A的玻璃化转变温度(或热挠曲温度)的约20℃以内,优选15℃内。向材料中添加填充物可以起提高材料玻璃化转变温度的作用。实际上,玻璃化转变温度以热挠曲温度表示。这儿公开的代表性的材料的热挠曲温度用材料的DMA软化点测定。As for thermal properties, build material A and support material B should have similar thermal deflection properties so that both materials can be successfully extruded into the same build chamber. As described in US Patent No. 5,866,058, the mold is built in a chamber heated to a temperature above the solidification temperature of a thermoplastic or other heat-curable modeling material, followed by gradual cooling to relieve the stress in the material. Stress is relieved from the model being built so that the finished model is stress-free and virtually deformation-free. As further recited in the '058 patent, the build material should have a glass transition temperature ( Tg ) above the build chamber temperature so that the pattern is not too soft to sag. The preferred temperature for the build cavity is therefore in the range between the solidification temperature of the molding material A and its creep relaxation temperature (the creep relaxation temperature is defined as the point at which the stress relaxation modulus decreases by a factor of 10 from its lower temperature limit). Likewise, the glass transition temperature of support material B should be higher than the temperature of the build chamber so that the support structure does not deform and maintain the structural fidelity of the model it supports. After testing, it is found that the glass transition temperature (or heat deflection temperature) of the support material B should be within about 20° C., preferably within 15° C., of the glass transition temperature (or heat deflection temperature) of the molding material A. Adding fillers to materials can act to increase the glass transition temperature of the material. In practice, glass transition temperature is expressed as heat deflection temperature. The heat deflection temperature of representative materials disclosed herein is determined by the DMA softening point of the material.
造型和支撑材料的组成Composition of molding and support materials
用PCT申请US01/41354号和PCT申请US00/17363号公开的型号的细丝供料分层堆积造型机试验本发明的材料。给出造型材料A和支撑材料B的下面的实例证实满足上面讨论的流变学标准。The materials of the present invention were tested using a filament-fed layered build-up molding machine of the type disclosed in PCT Application No. US01/41354 and PCT Application No. US00/17363. The following examples, given of build material A and support material B, demonstrate that the rheological criteria discussed above are met.
实例1Example 1
造型材料:造型材料A为聚碳酸酯树脂。一个具体的示例性聚碳酸酯树脂为(可从General ElectricPlastics获得)。这种树脂具有156℃的热挠曲温度,在1.2kg的负荷下300℃时熔体流动在20-30gms/10min范围内。聚碳酸酯树脂成功地从温度约320℃的液化器中挤出到温度约135℃的建造膛内。 Molding material : The molding material A is polycarbonate resin. A specific exemplary polycarbonate resin is (Available from General Electric Plastics). This resin has a heat deflection temperature of 156°C and a melt flow at 300°C under a load of 1.2kg in the range of 20-30 gms/10min. Polycarbonate resin was successfully extruded from a liquefier at about 320°C into a build chamber at about 135°C.
支撑材料:支撑材料B是包含聚亚苯基醚和聚烯烃,例如高冲击聚苯乙烯,的混合物的树脂。所需的重量百分比范围为约50-90%的聚亚苯基醚和约10-50%的聚烯烃。一个具体的树脂例子是75wt%的聚亚苯基醚和25wt%的高冲击聚苯乙烯(每种都可从General Electric Plastics获得)的混合物。这种树脂具有178℃的热挠曲温度和类似于造型材料的熔体流动。这种材料从温度约360℃的液化器中挤出,成功地形成使用聚碳酸酯树脂建造的模型的支撑结构。 Support material : Support material B is a resin comprising a mixture of polyphenylene ether and polyolefin, such as high impact polystyrene. The desired weight percent range is about 50-90% polyphenylene ether and about 10-50% polyolefin. A specific resin example is 75wt% polyphenylene ether and 25 wt% of A blend of high impact polystyrenes (each available from General Electric Plastics). This resin has a heat deflection temperature of 178°C and a melt flow similar to molding materials. Extruded from a liquefier at a temperature of around 360°C, the material successfully formed the support structure of the model built using polycarbonate resin.
实例2Example 2
造型材料:造型材料A为聚碳酸酯/丙烯腈-丁二烯-苯乙烯树脂。为了给材料提供聚碳酸酯的增强强度和韧性,树脂应该包含至少约50wt%的聚碳酸酯。一种特别的优选的聚碳酸酯/丙烯腈-丁二烯-苯乙烯树脂为(可从General Electric Plastics获得)。这种树脂具有143℃的热挠曲温度,在1.2kg的负荷下280℃时熔体流动在10-20gms/10min范围内。聚碳酸酯/丙烯腈-丁二烯-苯乙烯树脂成功地从温度约320℃的液化器中挤出到温度约110℃的建造膛内。 Molding material : The molding material A is polycarbonate/acrylonitrile-butadiene-styrene resin. To provide the material with the enhanced strength and toughness of polycarbonate, the resin should contain at least about 50% by weight polycarbonate. A particularly preferred polycarbonate/acrylonitrile-butadiene-styrene resin is (available from General Electric Plastics). This resin has a heat deflection temperature of 143°C and a melt flow at 280°C under a load of 1.2kg in the range of 10-20 gms/10min. The polycarbonate/acrylonitrile-butadiene-styrene resin was successfully extruded from a liquefier at about 320°C into a build chamber at about 110°C.
支撑材料:支撑材料B是包含聚亚苯基醚和聚烯烃,例如高冲击聚苯乙烯,的混合物的树脂。所需的重量百分比范围为约40-80%的聚亚苯基醚和约20-60%的聚烯烃。一个具体的树脂例子是(可从General Electric Plastics获得)聚亚苯基醚/聚苯乙烯混合物。这种树脂具有156℃的热挠曲温度和类似于造型材料的熔体流动。这种材料从温度约340℃的液化器中挤出,成功地形成使用聚碳酸酯/丙烯腈-丁二烯-苯乙烯树脂建造的模型的支撑结构。 Support material : Support material B is a resin comprising a mixture of polyphenylene ether and polyolefin, such as high impact polystyrene. The desired weight percent range is about 40-80% polyphenylene ether and about 20-60% polyolefin. A specific resin example is (available from General Electric Plastics) polyphenylene ether/polystyrene blend. This resin has a heat deflection temperature of 156°C and a melt flow similar to molding materials. Extruded from a liquefier at a temperature of around 340°C, the material was successfully formed into the support structure of a model built using polycarbonate/acrylonitrile-butadiene-styrene resin.
实例3Example 3
造型材料:造型材料A为聚苯砜树脂。一种具体的聚苯砜树脂的例子为(可从BP Amoco获得)。这种聚苯砜树脂具有236℃的热挠曲温度,在1.2kg的负荷下400℃时熔体流动在20-30gms/10min范围内。聚苯砜树脂成功地从温度约400℃的液化器中挤出到温度约200℃的建造膛内。 Modeling material : Modeling material A is polyphenylsulfone resin. An example of a specific polyphenylsulfone resin is (available from BP Amoco). This polyphenylsulfone resin has a heat deflection temperature of 236°C and a melt flow at 400°C under a load of 1.2kg in the range of 20-30 gms/10min. Polyphenylsulfone resin was successfully extruded from a liquefier at about 400°C into a build chamber at about 200°C.
支撑材料:支撑材料B是包含聚苯砜和无定形聚酰胺混合物的树脂。该材料可以进一步包含聚砜。所需的重量百分比范围为约60-90wt%的聚苯砜和约10-40wt%的无定形聚酰胺的混合物,或约60-90wt%的聚苯砜、约1-40wt%的聚砜和约10-40wt%的无定形聚酰胺的混合物。一个具体的示例性树脂是50wt%的聚苯砜(可从BP Amoco获得)、25wt%的聚砜(可从BP Amoco获得)和25wt%的EMS TR70无定形聚酰胺(可从瑞士的EMS-Chemie AG获得)的混合物。这种树脂具有224℃的热挠曲温度和类似于造型材料的熔体流动。这种材料从温度约350℃的液化器中挤出,成功地形成使用聚苯砜树脂建造的模型的支撑结构。使用聚合物化学中的常规技术复合该组分材料到支撑材料B。 Support material : Support material B is a resin comprising a mixture of polyphenylsulfone and amorphous polyamide. The material may further comprise polysulfone. The desired weight percent range is a mixture of about 60-90 wt % polyphenylsulfone and about 10-40 wt % amorphous polyamide, or about 60-90 wt % polyphenylsulfone, about 1-40 wt % polysulfone and about 10 wt % - 40% by weight of a mixture of amorphous polyamides. A specific exemplary resin is 50wt% Polyphenylsulfone (available from BP Amoco), 25 wt% of A mixture of polysulfone (available from BP Amoco) and 25% by weight of EMS TR70 amorphous polyamide (available from EMS-Chemie AG, Switzerland). This resin has a heat deflection temperature of 224°C and a melt flow similar to molding materials. Extruded from a liquefier at a temperature of about 350°C, the material successfully formed the support structure of a model built using polyphenylsulfone resin. The component materials were compounded to support material B using conventional techniques in polymer chemistry.
上面实例中给出的每种材料具有34MPa(5000psi)到83MPa(12000psi)的抗张强度、无定形聚合物的典型收缩(低于0.01cm/cm(0.010inch/inch))。上面实例的建造模型的每种材料和目前用于熔融堆积造型的材料相比具有更高的冲击强度、更大的韧性、更高的热挠曲温度和更好的化学稳定性。发现实例3建造模型的材料的韧性、冲击强度、耐热性和化学稳定性超过现有技术的任何迅速造型方法(rapidprototyping method)。Each of the materials given in the examples above has a tensile strength of 34 MPa (5000 psi) to 83 MPa (12000 psi), shrinkage typical of amorphous polymers (below 0.01 cm/cm (0.010 inch/inch)). Each of the materials used in the construction models of the above examples has higher impact strength, greater toughness, higher heat deflection temperature, and better chemical stability than materials currently used for fused deposition modeling. The toughness, impact strength, heat resistance and chemical stability of the material from which the Example 3 was built were found to exceed any rapid prototyping method of the prior art.
如上面提及的,造型材料A和支撑材料B可以包含惰性和/或活性填充材料。根据得到的模型的预定用途,填充物可以提供增强的材料性质。例如填充物能提供RF防护、传导、或无线电不穿透性质(对一些医疗应用有用)。填充物能选择性降低材料性质,但是这对一些应用是可接受的。例如向造型材料A或支撑材料B添加廉价的填充物可以降低这些材料的成本。填充物也能改变材料的热特性,例如填充物可以增加材料的耐热性,填充物可以减少材料在热固化时的收缩。典型的填充物包括玻璃纤维、碳纤维、炭黑、玻璃微球、碳酸钙、云母、滑石、硅土、氧化铝、碳化硅、钙硅石、石墨、金属和盐。在不出现不可接受地降低模型质量下向造型材料A和支撑材料B添加填充物材料的量的上限值为约20wt%。As mentioned above, the modeling material A and the support material B may contain inert and/or active filler materials. Depending on the intended use of the resulting model, fillers can provide enhanced material properties. For example fillers can provide RF protection, conduction, or radio-opaque properties (useful for some medical applications). Fillers can selectively degrade material properties, but this may be acceptable for some applications. For example, adding inexpensive fillers to the modeling material A or the support material B can reduce the cost of these materials. Fillers can also change the thermal properties of the material, for example, fillers can increase the heat resistance of the material, and fillers can reduce the shrinkage of the material during heat curing. Typical fillers include glass fibers, carbon fibers, carbon black, glass microspheres, calcium carbonate, mica, talc, silica, alumina, silicon carbide, wollastonite, graphite, metals and salts. The upper limit for the amount of filler material to be added to build material A and support material B without unacceptably reducing the quality of the model is about 20 wt%.
技术熟练的人员将认识到在本发明的造型和支撑材料中也可以使用无数的其它添加剂修整特定应用所需要的性质。例如添加增塑剂将降低材料的耐热性和熔体流动。添加染料和颜料可以改变材料的颜色。添加抗氧化剂减慢材料在挤压机中的热降解。而且可以向本发明的材料中添加少量的其它聚合物。在维持本发明的造型和支撑材料的基本流变学时填充物和其它添加剂的总量可以达到约30wt%。Those skilled in the art will recognize that a myriad of other additives may also be used in the styling and support materials of the present invention to tailor the properties desired for a particular application. For example, adding plasticizers will reduce the heat resistance and melt flow of the material. Adding dyes and pigments can change the color of a material. The addition of antioxidants slows down the thermal degradation of the material in the extruder. Also small amounts of other polymers may be added to the material of the invention. The total amount of fillers and other additives can be up to about 30% by weight while maintaining the basic rheology of the styling and support materials of the present invention.
造型和支撑材料A和B可以浇铸成棒状、粒状或其它形状用作造型原料,或可以在没有预先固化的情况下以液体原料使用。或者,混合物可以固化然后磨成粒状。粒状原料组合物可以经普通的挤出设备加工形成连续柔韧的细丝。希望地,这些细丝以连续的长度缠绕在线轴上,干燥。细丝一般直径很小,约0.178cm(0.070英寸),直径可以小到0.003cm(0.001英寸)。本发明的造型材料A和支撑材料B成功地形成造型细丝,在细丝供料堆积造型机中使用。The molding and support materials A and B can be cast into rods, pellets or other shapes for use as molding raw materials, or can be used as liquid raw materials without pre-curing. Alternatively, the mixture can be solidified and ground into granules. The granular raw material composition can be processed through common extrusion equipment to form continuous flexible filaments. Desirably, these filaments are wound on bobbins in continuous lengths and dried. The filaments are generally small in diameter, about 0.178 cm (0.070 inch), and can be as small as 0.003 cm (0.001 inch) in diameter. The molding material A and support material B of the present invention were successfully formed into molding filaments for use in a filament feed stacking molding machine.
要注意本发明的造型材料A和支撑材料B对水分敏感。已经证实这些材料暴露在潮湿的环境里将明显降低模型质量,因此维持干燥的条件是重要的。为了用熔融堆积技术将本发明的材料建造精确坚固的模型,材料必须干燥。引入本申请作为参考的PCT申请号US01/41354和PCT申请号US00/17363公开了使用本发明的高温、水分敏感的材料建造三维物体的特别合适的设备。‘363申请公开了一种带有高温建造膛的造型机,‘354申请公开了一种防潮细丝盒和在细丝供料堆积造型机中供应水分敏感造型细丝的细丝通道。It should be noted that the molding material A and supporting material B of the present invention are sensitive to moisture. It has been shown that exposure of these materials to moisture will significantly degrade the quality of the model, so it is important to maintain dry conditions. In order to construct accurate and robust patterns from the material of the present invention using the fused deposition technique, the material must be dry. PCT Application No. US01/41354 and PCT Application No. US00/17363, which are incorporated herein by reference, disclose particularly suitable apparatus for building three-dimensional objects using the high temperature, moisture sensitive materials of the present invention. The '363 application discloses a molding machine with a high temperature build chamber, and the '354 application discloses a moisture-resistant filament box and filament channel for supplying moisture sensitive molding filaments in a filament feed stack molding machine.
对于本发明的造型材料A和支撑材料B,可接受的水分含量(例如模型质量不被损坏的水平)为低于700ppm水含量的水平(使用Karl Fischer方法测定)。‘354申请公开了在细丝盒里供应细丝时干燥细丝的技术。一种干燥材料的方法为将包含材料的盒子放在真空、合适温度(一般在175-220°F)的炉子里直到达到需要的干度,此时要密封盒子不让水分进入。然后盒子被真空密封在不渗透水分的袋子里直至装到机器中。希望的干燥时间为4-8小时达到低于300ppm的水含量。另一种方法为将干燥剂的袋子放在盒子里干燥材料,不使用炉子。已经证实,将包含Tri-Sorb-分子筛和氧化钙(CaO)干燥剂的袋子放在盒子里,将盒子密封在不渗透水分的袋子里,干燥材料至水分含量低于700ppm,和干燥材料至优选范围100-400ppm。合适的Tri-Sorb-分子筛干燥剂包括下列这些:NaA沸石、KA沸石、CaA沸石、NaX沸石和铝硅酸镁。For the molding material A and support material B of the present invention, acceptable moisture content (eg, a level at which the quality of the model is not impaired) is a level below 700 ppm water content (determined using the Karl Fischer method). The '354 application discloses techniques for drying the filament as it is supplied in a filament cassette. One method of drying the material is to place the box containing the material in a vacuum oven at a suitable temperature (typically 175-220°F) until the desired dryness is achieved, at which point the box is sealed to keep moisture out. The boxes are then vacuum sealed in moisture-impermeable bags until loaded into the machine. The desired drying time is 4-8 hours to achieve a water content below 300 ppm. Another method is to place the bag of desiccant in the box to dry the material without using the oven. It has been demonstrated that placing bags containing Tri-Sorb-Molecular Sieve and Calcium Oxide (CaO) desiccant in a box, sealing the box in a moisture-impermeable bag, dries the material to a moisture content below 700ppm, and dries the material to preferably Range 100-400ppm. Suitable Tri-Sorb-molecular sieve desiccants include the following: NaA zeolite, KA zeolite, CaA zeolite, NaX zeolite and magnesium aluminosilicate.
用本发明的材料制成的模型比现有技术使用的材料制成的模型更加有用。例如用本发明的材料制成的模型可以用作动力工具和家用电器的功能部件,其强度和韧性是很重要的;汽车应用的功能部件,其强度、韧性、高耐热性和化学稳定性是很重要的;医疗和牙科设备的功能部件,该部件在重复的蒸汽消毒后必须保持关键性质;一些需要低的可燃性和发烟性的应用的功能部件。Models made of the material of the present invention are more useful than models made of materials used in the prior art. For example, models made of the material of the present invention can be used as functional parts of power tools and household appliances, where strength and toughness are important; functional parts for automotive applications, where strength, toughness, high heat resistance and chemical stability It is very important; functional parts of medical and dental equipment, which must maintain critical properties after repeated steam sterilization; some functional parts of applications requiring low flammability and smoke generation.
应该注意,虽然这里将本发明的材料称为“造型”或“支撑”材料,但是这些材料可以相互转变,用所谓的“支撑”材料制成模型,用所谓的“造型”材料制成模型的支撑结构。这里描述为造型材料的材料的性质对大部分应用来说比支撑材料优异。例如,用这里作为造型材料介绍的材料建成的模型比用这儿作为支撑材料介绍的材料建成的模型更强更坚固。根据材料的预期的典型使用,为了方便指定,将这里的材料分类为“造型”或“支撑”材料。It should be noted that although the materials of the present invention are referred to herein as "model" or "support" materials, these materials can be transformed into one another, with so-called "support" materials used to form models and so-called "model" materials used to form the model's supporting structure. The properties of materials described herein as build materials are superior to support materials for most applications. For example, models built with materials described here as modeling materials are stronger and stronger than models built with materials described here as support materials. Materials herein are classified, for convenience of designation, as either "model" or "support" materials, depending on their intended typical use.
尽管本发明参照优选方案描述本发明,本领域的熟练人员将认识到在不脱离本发明发明的精神和范围的情况下可以进行形式和细节上的改变。Although the present invention has been described with reference to preferred embodiments, workers skilled in the art will recognize that changes may be made in form and detail without departing from the spirit and scope of the invention.
Claims (14)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/854,220 | 2001-05-11 | ||
US09/854,220 US6645412B2 (en) | 1999-04-20 | 2001-05-11 | Process of making a three-dimensional object |
PCT/US2002/011714 WO2002093360A1 (en) | 2001-05-11 | 2002-04-15 | Materials and method for three-dimensional modeling |
Publications (2)
Publication Number | Publication Date |
---|---|
CN1552017A CN1552017A (en) | 2004-12-01 |
CN1552017B true CN1552017B (en) | 2010-10-06 |
Family
ID=25318067
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN028096924A Expired - Lifetime CN1552017B (en) | 2001-05-11 | 2002-04-15 | Material and method for three-dimensional modeling |
Country Status (7)
Country | Link |
---|---|
US (1) | US6645412B2 (en) |
EP (1) | EP1388051B1 (en) |
JP (1) | JP4256170B2 (en) |
KR (1) | KR100890598B1 (en) |
CN (1) | CN1552017B (en) |
HK (1) | HK1067905A1 (en) |
WO (1) | WO2002093360A1 (en) |
Families Citing this family (146)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6776602B2 (en) * | 1999-04-20 | 2004-08-17 | Stratasys, Inc. | Filament cassette and loading system |
US7754807B2 (en) * | 1999-04-20 | 2010-07-13 | Stratasys, Inc. | Soluble material and process for three-dimensional modeling |
US7314591B2 (en) | 2001-05-11 | 2008-01-01 | Stratasys, Inc. | Method for three-dimensional modeling |
US6722872B1 (en) * | 1999-06-23 | 2004-04-20 | Stratasys, Inc. | High temperature modeling apparatus |
US6866807B2 (en) * | 2001-09-21 | 2005-03-15 | Stratasys, Inc. | High-precision modeling filament |
CA2378922C (en) * | 2002-01-16 | 2009-01-27 | Rutgers, The State University Of New Jersey | Compositions and methods of making plastic articles from polymer blends containing polyethylene |
EP2295227A3 (en) | 2002-12-03 | 2018-04-04 | Stratasys Ltd. | Apparatus and method for printing of three-dimensional objects |
ATE384761T1 (en) * | 2002-12-17 | 2008-02-15 | Solvay Advanced Polymers Llc | 4,4'-BIPHENOL POLYSULFONE COMPOSITIONS, PRODUCTION METHOD THEREFOR AND ARTICLES THEREOF |
US6869559B2 (en) * | 2003-05-05 | 2005-03-22 | Stratasys, Inc. | Material and method for three-dimensional modeling |
GB2415374A (en) * | 2004-06-25 | 2005-12-28 | Leuven K U Res & Dev | Targeted delivery of biologically active substances using iron oxide/gold core-shell nanoparticles |
US7236166B2 (en) * | 2005-01-18 | 2007-06-26 | Stratasys, Inc. | High-resolution rapid manufacturing |
US20080020049A1 (en) * | 2005-02-25 | 2008-01-24 | Andrew Darling | Super-sparger microcarrier beads and precision extrusion deposited poly-epsilon-caprolactone structures for biological applications |
US7341214B2 (en) * | 2005-06-30 | 2008-03-11 | Stratasys, Inc. | Cassette spool lock |
US7384255B2 (en) * | 2005-07-01 | 2008-06-10 | Stratasys, Inc. | Rapid prototyping system with controlled material feedstock |
JP4807005B2 (en) * | 2005-08-19 | 2011-11-02 | テクノポリマー株式会社 | FDM or SLS thermoplastic resin composition and molding |
US7680555B2 (en) * | 2006-04-03 | 2010-03-16 | Stratasys, Inc. | Auto tip calibration in an extrusion apparatus |
US7604470B2 (en) * | 2006-04-03 | 2009-10-20 | Stratasys, Inc. | Single-motor extrusion head having multiple extrusion lines |
US7403833B2 (en) * | 2006-04-03 | 2008-07-22 | Stratasys, Inc. | Method for optimizing spatial orientations of computer-aided design models |
US20100209875A1 (en) * | 2006-04-12 | 2010-08-19 | Heraeus | Method and device(s) for production of dental prostheses |
US20080006966A1 (en) * | 2006-07-07 | 2008-01-10 | Stratasys, Inc. | Method for building three-dimensional objects containing metal parts |
US7910041B1 (en) * | 2006-11-27 | 2011-03-22 | Stratasys, Inc. | Build materials containing nanofibers for use with extrusion-based layered depositions systems |
US8765045B2 (en) * | 2007-01-12 | 2014-07-01 | Stratasys, Inc. | Surface-treatment method for rapid-manufactured three-dimensional objects |
JP5039795B2 (en) * | 2007-02-12 | 2012-10-03 | ストラタシス,インコーポレイテッド | Viscous pump for extrusion deposition systems. |
US20090295032A1 (en) * | 2007-03-14 | 2009-12-03 | Stratasys, Inc. | Method of building three-dimensional object with modified ABS materials |
US8050786B2 (en) * | 2007-07-11 | 2011-11-01 | Stratasys, Inc. | Method for building three-dimensional objects with thin wall regions |
US7625200B2 (en) * | 2007-07-31 | 2009-12-01 | Stratasys, Inc. | Extrusion head for use in extrusion-based layered deposition modeling |
US7896209B2 (en) | 2008-04-30 | 2011-03-01 | Stratasys, Inc. | Filament drive mechanism for use in extrusion-based digital manufacturing systems |
US7897074B2 (en) * | 2008-04-30 | 2011-03-01 | Stratasys, Inc. | Liquefier assembly for use in extrusion-based digital manufacturing systems |
US8155775B2 (en) * | 2008-10-02 | 2012-04-10 | Stratasys, Inc. | Support structure packaging |
US8246888B2 (en) * | 2008-10-17 | 2012-08-21 | Stratasys, Inc. | Support material for digital manufacturing systems |
US20100161105A1 (en) * | 2008-12-22 | 2010-06-24 | Stratasys, Inc. | Combined process for building three-dimensional models |
EP2408862B1 (en) | 2009-03-19 | 2015-02-18 | Stratasys, Inc. | Biobased polymer compositions |
CN102596543B (en) * | 2009-06-23 | 2014-09-17 | 斯特拉塔西斯公司 | Consumable materials having customized characteristics |
CN102149859B (en) | 2009-06-25 | 2015-08-26 | 北京阿迈特医疗器械有限公司 | For the preparation of the method and apparatus of three-dimensional porous tubular bracket |
US8349239B2 (en) * | 2009-09-23 | 2013-01-08 | Stratasys, Inc. | Seam concealment for three-dimensional models |
US8236227B2 (en) * | 2009-09-30 | 2012-08-07 | Stratasys, Inc. | Method for building three-dimensional models in extrusion-based digital manufacturing systems using tracked filaments |
US8221669B2 (en) | 2009-09-30 | 2012-07-17 | Stratasys, Inc. | Method for building three-dimensional models in extrusion-based digital manufacturing systems using ribbon filaments |
US8439665B2 (en) * | 2009-09-30 | 2013-05-14 | Stratasys, Inc. | Ribbon liquefier for use in extrusion-based digital manufacturing systems |
EP2501535B1 (en) | 2009-11-19 | 2017-11-15 | Stratasys, Inc. | Encoded consumable filaments for use in additive manufacturing systems |
US20110117268A1 (en) * | 2009-11-19 | 2011-05-19 | Stratasys, Inc. | Consumable materials having encoded markings for use with direct digital manufacturing systems |
EP2521625A2 (en) * | 2010-01-05 | 2012-11-14 | Stratasys, Inc. | Support cleaning system |
US8983643B2 (en) * | 2010-01-15 | 2015-03-17 | Stratasys, Inc. | Method for generating and building support structures with deposition-based digital manufacturing systems |
US9022769B2 (en) | 2010-07-22 | 2015-05-05 | Stratasys, Inc. | Multiple-zone liquefier assembly for extrusion-based additive manufacturing systems |
WO2012037329A2 (en) | 2010-09-17 | 2012-03-22 | Stratasys, Inc. | Semi-crystalline consumable materials for use in extrusion-based additive manufacturing systems |
US8920697B2 (en) | 2010-09-17 | 2014-12-30 | Stratasys, Inc. | Method for building three-dimensional objects in extrusion-based additive manufacturing systems using core-shell consumable filaments |
US8647098B2 (en) | 2010-09-22 | 2014-02-11 | Stratasys, Inc. | Liquefier assembly for use in extrusion-based additive manufacturing systems |
US8815141B2 (en) | 2010-09-22 | 2014-08-26 | Stratasys, Inc. | Method for building three-dimensional models with extrusion-based additive manufacturing systems |
US8647102B2 (en) | 2010-12-22 | 2014-02-11 | Stratasys, Inc. | Print head assembly and print head for use in fused deposition modeling system |
US8419996B2 (en) | 2010-12-22 | 2013-04-16 | Stratasys, Inc. | Print head assembly for use in fused deposition modeling system |
US9238329B2 (en) | 2010-12-22 | 2016-01-19 | Stratasys, Inc. | Voice coil mechanism for use in additive manufacturing system |
US8663533B2 (en) | 2010-12-22 | 2014-03-04 | Stratasys, Inc. | Method of using print head assembly in fused deposition modeling system |
US8460755B2 (en) | 2011-04-07 | 2013-06-11 | Stratasys, Inc. | Extrusion-based additive manufacturing process with part annealing |
WO2012151494A2 (en) | 2011-05-05 | 2012-11-08 | Interfacial Solutions Ip, Llc | Radiation curable polymers |
DE102011075540A1 (en) * | 2011-05-10 | 2012-11-15 | Evonik Röhm Gmbh | Multicolored fused deposition modeling printing |
US8459280B2 (en) | 2011-09-23 | 2013-06-11 | Stratasys, Inc. | Support structure removal system |
US9114571B2 (en) * | 2011-10-27 | 2015-08-25 | Solidscape, Inc. | Method for reducing stress in three dimensional model |
US9073263B2 (en) | 2011-12-22 | 2015-07-07 | Stratasys, Inc. | Spool assembly for additive manufacturing system, and methods of manufacture and use thereof |
US9321608B2 (en) | 2011-12-22 | 2016-04-26 | Stratasys, Inc. | Spool assembly with locking mechanism for additive manufacturing system, and methods of use thereof |
US8985497B2 (en) | 2011-12-22 | 2015-03-24 | Stratasys, Inc. | Consumable assembly with payout tube for additive manufacturing system |
US9050788B2 (en) | 2011-12-22 | 2015-06-09 | Stratasys, Inc. | Universal adapter for consumable assembly used with additive manufacturing system |
JP5772668B2 (en) * | 2012-03-08 | 2015-09-02 | カシオ計算機株式会社 | Three-dimensional modeling method, three-dimensional modeling complex, and three-dimensional modeling apparatus |
US9050753B2 (en) | 2012-03-16 | 2015-06-09 | Stratasys, Inc. | Liquefier assembly having inlet liner for use in additive manufacturing system |
US9364986B1 (en) | 2012-05-22 | 2016-06-14 | Rapid Prototype and Manufacturing LLC | Method for three-dimensional manufacturing and high density articles produced thereby |
US9708457B2 (en) | 2012-06-28 | 2017-07-18 | Stratasys, Inc. | Moisture scavenger composition |
US9327350B2 (en) | 2012-08-16 | 2016-05-03 | Stratasys, Inc. | Additive manufacturing technique for printing three-dimensional parts with printed receiving surfaces |
US10029415B2 (en) | 2012-08-16 | 2018-07-24 | Stratasys, Inc. | Print head nozzle for use with additive manufacturing system |
US11020899B2 (en) | 2012-08-16 | 2021-06-01 | Stratasys, Inc. | Additive manufacturing system with extended printing volume, and methods of use thereof |
US9636868B2 (en) | 2012-08-16 | 2017-05-02 | Stratasys, Inc. | Additive manufacturing system with extended printing volume, and methods of use thereof |
US9168697B2 (en) | 2012-08-16 | 2015-10-27 | Stratasys, Inc. | Additive manufacturing system with extended printing volume, and methods of use thereof |
US9511547B2 (en) | 2012-08-16 | 2016-12-06 | Stratasys, Inc. | Method for printing three-dimensional parts with additive manufacturing systems using scaffolds |
US9174388B2 (en) | 2012-08-16 | 2015-11-03 | Stratasys, Inc. | Draw control for extrusion-based additive manufacturing systems |
WO2014072148A1 (en) * | 2012-11-09 | 2014-05-15 | Evonik Industries Ag | Use and production of coated filaments for extrusion-based 3d printing processes |
US12064917B2 (en) | 2012-11-21 | 2024-08-20 | Stratasys, Inc. | Method for printing three-dimensional parts with cyrstallization kinetics control |
US9592530B2 (en) | 2012-11-21 | 2017-03-14 | Stratasys, Inc. | Additive manufacturing with polyamide consumable materials |
US9744722B2 (en) | 2012-11-21 | 2017-08-29 | Stratasys, Inc. | Additive manufacturing with polyamide consumable materials |
US9527242B2 (en) | 2012-11-21 | 2016-12-27 | Stratasys, Inc. | Method for printing three-dimensional parts wtih crystallization kinetics control |
US9233506B2 (en) | 2012-12-07 | 2016-01-12 | Stratasys, Inc. | Liquefier assembly for use in additive manufacturing system |
US9321609B2 (en) | 2012-12-07 | 2016-04-26 | Stratasys, Inc. | Filament drive mechanism for use in additive manufacturing system |
US9090428B2 (en) | 2012-12-07 | 2015-07-28 | Stratasys, Inc. | Coil assembly having permeable hub |
US8961167B2 (en) | 2012-12-21 | 2015-02-24 | Stratasys, Inc. | Automated additive manufacturing system for printing three-dimensional parts, printing farm thereof, and method of use thereof |
US9216544B2 (en) | 2012-12-21 | 2015-12-22 | Stratasys, Inc. | Automated additive manufacturing system for printing three-dimensional parts, printing farm thereof, and method of use thereof |
US9399320B2 (en) | 2013-03-08 | 2016-07-26 | Stratasys, Inc. | Three-dimensional parts having interconnected hollow patterns, and method for generating and printing thereof |
US9421713B2 (en) | 2013-03-08 | 2016-08-23 | Stratasys, Inc. | Additive manufacturing method for printing three-dimensional parts with purge towers |
US10093039B2 (en) | 2013-03-08 | 2018-10-09 | Stratasys, Inc. | Three-dimensional parts having interconnected Hollow patterns, method of manufacturing and method of producing composite part |
CN105408091B (en) * | 2013-03-14 | 2018-12-18 | 斯特拉塔西斯公司 | Ceramic support structure |
US9527240B2 (en) | 2013-03-15 | 2016-12-27 | Stratasys, Inc. | Additive manufacturing system and method for printing three-dimensional parts using velocimetry |
US9802360B2 (en) | 2013-06-04 | 2017-10-31 | Stratsys, Inc. | Platen planarizing process for additive manufacturing system |
US9523934B2 (en) | 2013-07-17 | 2016-12-20 | Stratasys, Inc. | Engineering-grade consumable materials for electrophotography-based additive manufacturing |
US9714318B2 (en) | 2013-07-26 | 2017-07-25 | Stratasys, Inc. | Polyglycolic acid support material for additive manufacturing systems |
CN105555867B (en) * | 2013-09-11 | 2018-08-24 | 东丽株式会社 | Heat fusing laminated type three-dimensional modeling raw material and heat fusing laminated type 3D printing equipment filiform |
US9950474B2 (en) | 2013-09-13 | 2018-04-24 | Statasys, Inc. | Additive manufacturing system and process with precision substractive technique |
US10131131B2 (en) | 2013-10-04 | 2018-11-20 | Stratasys, Inc. | Liquefier assembly with multiple-zone plate heater assembly |
US10201931B2 (en) | 2013-10-04 | 2019-02-12 | Stratasys, Inc. | Additive manufacturing system and process with material flow feedback control |
US10086564B2 (en) | 2013-10-04 | 2018-10-02 | Stratsys, Inc. | Additive manufacturing process with dynamic heat flow control |
US9327447B2 (en) | 2013-10-04 | 2016-05-03 | Stratasys, Inc. | Liquefier assembly for additive manufacturing systems, and methods of use thereof |
WO2015061855A1 (en) * | 2013-10-30 | 2015-05-07 | Laing O'rourke Australia Pty Limited | Method for fabricating an object |
US10843401B2 (en) * | 2013-11-01 | 2020-11-24 | Kraton Polymers U.S. Llc | Fuse molded three dimensional article and a method for making the same |
US9744730B2 (en) | 2013-11-22 | 2017-08-29 | Stratasys, Inc. | Magnetic platen assembly for additive manufacturing system |
US11130276B2 (en) | 2013-12-18 | 2021-09-28 | Ineos Styrolution Group Gmbh | Use of molding materials based on vinyl aromatic/diene block copolymers for 3-D-printing |
US20150183159A1 (en) * | 2013-12-30 | 2015-07-02 | Chad E. Duty | Large scale room temperature polymer advanced manufacturing |
CN103756236B (en) * | 2014-01-06 | 2017-01-11 | 朱叶周 | Thermoplastic elastomer composition for preparing flexible printing material for three-dimensional printing rapid prototyping |
US9650537B2 (en) | 2014-04-14 | 2017-05-16 | Ut-Battelle, Llc | Reactive polymer fused deposition manufacturing |
US20170144368A1 (en) * | 2014-06-16 | 2017-05-25 | Sabic Global Technologies B.V. | Process for additive manufacturing using thermoplastic materials having selected melt indexes |
KR102368335B1 (en) * | 2014-07-22 | 2022-02-28 | 바스프 에스이 | Mixture for use in a fused filament fabrication process |
US10059053B2 (en) | 2014-11-04 | 2018-08-28 | Stratasys, Inc. | Break-away support material for additive manufacturing |
JP6700745B2 (en) * | 2014-11-28 | 2020-05-27 | キヤノン株式会社 | Powder, thermoplastic composition, and method for producing three-dimensional object |
WO2016084928A1 (en) * | 2014-11-28 | 2016-06-02 | キヤノン株式会社 | Powder, thermoplastic composition, and method for manufacturing three-dimensional object |
US9694545B2 (en) | 2014-12-18 | 2017-07-04 | Stratasys, Inc. | Remotely-adjustable purge station for use in additive manufacturing systems |
WO2016095059A1 (en) * | 2014-12-19 | 2016-06-23 | Hirschberg Engineering | Method and apparatus for the layer-by-layer production of molded articles |
US9610733B2 (en) | 2015-01-06 | 2017-04-04 | Stratasys, Inc. | Additive manufacturing with soluble build sheet and part marking |
EP3245255B1 (en) * | 2015-01-12 | 2019-05-15 | PolyOne Corporation | Support material for 3d printing of polymer compounds |
US10400080B2 (en) | 2015-03-16 | 2019-09-03 | Sabic Global Technologies B.V. | Fibrillated polymer compositions and methods of their manufacture |
WO2016171191A1 (en) | 2015-04-20 | 2016-10-27 | Mcppイノベーション合同会社 | Shaping filament for material extrusion type three-dimensional printer, and process for producing shaped object |
EP3310843B1 (en) | 2015-06-19 | 2024-09-18 | Stratasys, Inc. | Water dispersible polymer for use in additive manufacturing |
EP3313617B1 (en) | 2015-06-25 | 2023-06-14 | 3M Innovative Properties Company | Methods of making metal bond abrasive articles and metal bond abrasive articles |
CN105150542A (en) * | 2015-09-29 | 2015-12-16 | 合肥中加激光技术有限公司 | Extrusion spray-head structure of FDM (Fused Deposition Modeling) 3D printer |
US10399326B2 (en) | 2015-10-30 | 2019-09-03 | Stratasys, Inc. | In-situ part position measurement |
WO2017083382A1 (en) | 2015-11-12 | 2017-05-18 | 3M Innovative Properties Company | A method of and system for building up a dental object |
CN108348311A (en) | 2015-11-13 | 2018-07-31 | 株式会社理光 | The manufacturing device of three-dimensionally shaped material group, the manufacturing method and three-dimensionally shaped object of three-dimensionally shaped object |
JP6603807B2 (en) * | 2015-12-03 | 2019-11-06 | ブキャナン エル.スティーブン | Radiopaque 3D printing ink |
WO2017100451A1 (en) * | 2015-12-11 | 2017-06-15 | Sabic Global Technologies B.V. | Method of additive manufacturing to make objects having improved and tailored properties |
CN108290345A (en) * | 2015-12-11 | 2018-07-17 | 沙特基础工业全球技术有限公司 | Increasing material manufacturing method for improving interlayer adhesion force |
US10144011B2 (en) | 2015-12-17 | 2018-12-04 | United Technologies Corporation | System for powder heat treatment and classification via fluidized bed |
CN109071802B (en) * | 2016-04-01 | 2021-07-13 | 索尔维特殊聚合物美国有限责任公司 | Method for producing a three-dimensional object |
US10427353B2 (en) * | 2016-05-13 | 2019-10-01 | Ricoh Company, Ltd. | Additive manufacturing using stimuli-responsive high-performance polymers |
WO2017223276A1 (en) | 2016-06-24 | 2017-12-28 | Polyone Corporation | Coc polymer compounds for 3d printing |
CN107803982B (en) * | 2016-09-06 | 2020-05-12 | 珠海赛纳打印科技股份有限公司 | Printing method and device for 3D object with suspension structure |
JP2019529182A (en) * | 2016-09-22 | 2019-10-17 | ストラタシス リミテッド | Method and system for solid freeform fabrication |
WO2018055522A1 (en) | 2016-09-22 | 2018-03-29 | Stratasys Ltd. | Formulation, method and system for solid freeform fabrication |
US11440261B2 (en) | 2016-11-08 | 2022-09-13 | The Boeing Company | Systems and methods for thermal control of additive manufacturing |
US10084615B2 (en) * | 2016-11-14 | 2018-09-25 | Electronics And Telecommunications Research Institute | Handover method and control transfer method |
WO2018158426A1 (en) * | 2017-03-02 | 2018-09-07 | Bond High Performance 3D Technology B.V. | Object made by additive manufacturing and method to produce said object |
USD888115S1 (en) | 2017-03-16 | 2020-06-23 | Stratasys, Inc. | Nozzle |
WO2018197156A1 (en) | 2017-04-24 | 2018-11-01 | Solvay Specialty Polymers Usa, Llc | Method of making a three-dimensional object using ppsu |
US20200384681A1 (en) | 2017-04-24 | 2020-12-10 | Solvay Specialty Polymers Usa, Llc | Method of making a three-dimensional object using ppsu |
DE102017210146A1 (en) * | 2017-06-19 | 2018-12-20 | Bayerische Motoren Werke Aktiengesellschaft | Apparatus and method for the additive production of a molded part of granules |
US11851763B2 (en) * | 2017-06-23 | 2023-12-26 | General Electric Company | Chemical vapor deposition during additive manufacturing |
WO2019063740A1 (en) * | 2017-09-28 | 2019-04-04 | Rhodia Operations | Method for manufacturing a three-dimensional object using polyamide based support material |
EP3694939A1 (en) | 2017-10-10 | 2020-08-19 | Stratasys, Inc. | Water-dispersible thermoplastic material comprising sulfonated copolymer for use in additive manufacturing |
JP7184079B2 (en) * | 2018-04-26 | 2022-12-06 | 三菱ケミカル株式会社 | Materials for polyamide-based 3D printers |
US11247387B2 (en) | 2018-08-30 | 2022-02-15 | Stratasys, Inc. | Additive manufacturing system with platen having vacuum and air bearing |
WO2020077127A1 (en) | 2018-10-10 | 2020-04-16 | Stratasys, Inc. | Water dispersible sulfonated thermoplastic copolymer for use in additive manufacturing |
CA3182234A1 (en) | 2020-06-10 | 2021-12-16 | Gregory ELLSON | Materials for photoinitiated cationic ring-opening polymerization and uses thereof |
US20230271381A1 (en) * | 2020-08-03 | 2023-08-31 | Chromatic 3D Materials, Inc. | Method for three dimensional printing using lead-in and lead-out blocks |
US12157800B2 (en) | 2021-04-12 | 2024-12-03 | Stratasys, Inc. | Method for underwater processing of water-dispersible materials |
EP4457057A1 (en) | 2021-12-30 | 2024-11-06 | Saint-Gobain Abrasives, Inc. | Abrasive articles and methods for forming same |
Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1050886A (en) * | 1989-10-13 | 1991-04-24 | 出光兴产株式会社 | Styrene polymer composition |
US5059266A (en) * | 1989-05-23 | 1991-10-22 | Brother Kogyo Kabushiki Kaisha | Apparatus and method for forming three-dimensional article |
CN1139611A (en) * | 1995-07-04 | 1997-01-08 | 斯特拉特西斯公司 | Process and apparatus of support removal for three-dimensional modeling |
US5738817A (en) * | 1996-02-08 | 1998-04-14 | Rutgers, The State University | Solid freeform fabrication methods |
US5932055A (en) * | 1997-11-11 | 1999-08-03 | Rockwell Science Center Llc | Direct metal fabrication (DMF) using a carbon precursor to bind the "green form" part and catalyze a eutectic reducing element in a supersolidus liquid phase sintering (SLPS) process |
US6119567A (en) * | 1997-07-10 | 2000-09-19 | Ktm Industries, Inc. | Method and apparatus for producing a shaped article |
US6165406A (en) * | 1999-05-27 | 2000-12-26 | Nanotek Instruments, Inc. | 3-D color model making apparatus and process |
US6214279B1 (en) * | 1999-10-02 | 2001-04-10 | Nanotek Instruments, Inc. | Apparatus and process for freeform fabrication of composite reinforcement preforms |
US6228923B1 (en) * | 1997-04-02 | 2001-05-08 | Stratasys, Inc. | Water soluble rapid prototyping support and mold material |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3445570A1 (en) * | 1984-12-14 | 1986-06-19 | Basf Ag, 6700 Ludwigshafen | SELF-EXTINGUISHING THERMOPLASTIC POLYESTER MOLDS |
JP2597778B2 (en) * | 1991-01-03 | 1997-04-09 | ストラタシイス,インコーポレイテッド | Three-dimensional object assembling system and assembling method |
JPH06122815A (en) * | 1992-10-13 | 1994-05-06 | Sanko Chem Co Ltd | Polyamide resin composition |
US5503785A (en) | 1994-06-02 | 1996-04-02 | Stratasys, Inc. | Process of support removal for fused deposition modeling |
JPH08281808A (en) * | 1995-04-17 | 1996-10-29 | Ricoh Co Ltd | Manufacture of stereoscopic shape |
DE69628348T2 (en) * | 1995-09-27 | 2004-06-09 | 3D Systems, Inc., Valencia | Method and device for changing data and system control in a modeling device by selective material deposition |
US6070107A (en) | 1997-04-02 | 2000-05-30 | Stratasys, Inc. | Water soluble rapid prototyping support and mold material |
US6067480A (en) | 1997-04-02 | 2000-05-23 | Stratasys, Inc. | Method and apparatus for in-situ formation of three-dimensional solid objects by extrusion of polymeric materials |
TW500765B (en) * | 1998-05-13 | 2002-09-01 | Sumitomo Chemical Co | Thermoplastic resin composition and heat-resistant tray for IC |
US6322728B1 (en) | 1998-07-10 | 2001-11-27 | Jeneric/Pentron, Inc. | Mass production of dental restorations by solid free-form fabrication methods |
KR100291953B1 (en) * | 1999-03-15 | 2001-06-01 | 윤덕용 | Variable deposition manufacturing method and apparatus |
CN1320992C (en) | 1999-04-20 | 2007-06-13 | 斯特拉塔西斯公司 | Soluble material and process for three-dimensional modeling |
EP1204517B1 (en) | 1999-06-23 | 2009-04-29 | Stratasys, Inc. | High temperature modeling apparatus |
JP4451942B2 (en) * | 1999-08-26 | 2010-04-14 | ダイセル化学工業株式会社 | Styrenic resin composition |
JP2001098172A (en) * | 1999-09-29 | 2001-04-10 | Sumitomo Chem Co Ltd | Thermoplastic resin composition |
-
2001
- 2001-05-11 US US09/854,220 patent/US6645412B2/en not_active Expired - Lifetime
-
2002
- 2002-04-15 EP EP02723850.0A patent/EP1388051B1/en not_active Expired - Lifetime
- 2002-04-15 CN CN028096924A patent/CN1552017B/en not_active Expired - Lifetime
- 2002-04-15 KR KR1020037014482A patent/KR100890598B1/en not_active IP Right Cessation
- 2002-04-15 JP JP2002589969A patent/JP4256170B2/en not_active Expired - Fee Related
- 2002-04-15 WO PCT/US2002/011714 patent/WO2002093360A1/en active Application Filing
-
2005
- 2005-02-15 HK HK05101184.9A patent/HK1067905A1/en not_active IP Right Cessation
Patent Citations (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5059266A (en) * | 1989-05-23 | 1991-10-22 | Brother Kogyo Kabushiki Kaisha | Apparatus and method for forming three-dimensional article |
CN1050886A (en) * | 1989-10-13 | 1991-04-24 | 出光兴产株式会社 | Styrene polymer composition |
CN1139611A (en) * | 1995-07-04 | 1997-01-08 | 斯特拉特西斯公司 | Process and apparatus of support removal for three-dimensional modeling |
US5738817A (en) * | 1996-02-08 | 1998-04-14 | Rutgers, The State University | Solid freeform fabrication methods |
US5900207A (en) * | 1996-02-08 | 1999-05-04 | Rutgers, The State University Old Queens | Solid freeform fabrication methods |
US6228923B1 (en) * | 1997-04-02 | 2001-05-08 | Stratasys, Inc. | Water soluble rapid prototyping support and mold material |
US6119567A (en) * | 1997-07-10 | 2000-09-19 | Ktm Industries, Inc. | Method and apparatus for producing a shaped article |
US5932055A (en) * | 1997-11-11 | 1999-08-03 | Rockwell Science Center Llc | Direct metal fabrication (DMF) using a carbon precursor to bind the "green form" part and catalyze a eutectic reducing element in a supersolidus liquid phase sintering (SLPS) process |
US6165406A (en) * | 1999-05-27 | 2000-12-26 | Nanotek Instruments, Inc. | 3-D color model making apparatus and process |
US6214279B1 (en) * | 1999-10-02 | 2001-04-10 | Nanotek Instruments, Inc. | Apparatus and process for freeform fabrication of composite reinforcement preforms |
Non-Patent Citations (1)
Title |
---|
CN 1139611 A,全文. |
Also Published As
Publication number | Publication date |
---|---|
HK1067905A1 (en) | 2005-04-22 |
US20020017743A1 (en) | 2002-02-14 |
WO2002093360A1 (en) | 2002-11-21 |
JP2004532753A (en) | 2004-10-28 |
KR20040034605A (en) | 2004-04-28 |
EP1388051B1 (en) | 2016-12-21 |
EP1388051A1 (en) | 2004-02-11 |
JP4256170B2 (en) | 2009-04-22 |
CN1552017A (en) | 2004-12-01 |
EP1388051A4 (en) | 2009-02-11 |
KR100890598B1 (en) | 2009-03-25 |
US6645412B2 (en) | 2003-11-11 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN1552017B (en) | Material and method for three-dimensional modeling | |
JP4224456B2 (en) | Method for 3D modeling | |
US6869559B2 (en) | Material and method for three-dimensional modeling | |
JP2004532753A5 (en) | Method for 3D modeling | |
CN110023010A (en) | Stress relaxation in the part of increasing material manufacturing | |
CN110049838A (en) | Increasing material manufacturing with the supply of thermal flexure material | |
KR101727123B1 (en) | Additive manufacturing with polyamide consumable materials | |
JP2018519198A (en) | Method for manufacturing a 3D object | |
JPWO2019208741A1 (en) | Polyamide-based 3D printer material | |
JP7335600B2 (en) | POWDER MATERIAL FOR THREE-DIMENSIONAL PRODUCTION, THREE-DIMENSIONAL PRODUCT AND METHOD FOR MANUFACTURING THREE-DIMENSIONAL PRODUCT | |
KR101764237B1 (en) | Crystallized polylactic acid filament, production method thereof, and method and fdm 3d printer for producing 3d output using the same | |
JPWO2018074373A1 (en) | Three-dimensional modeling composition, three-dimensional modeling manufacturing method, and three-dimensional modeling | |
JP7136186B2 (en) | Method for producing thermoplastic resin-containing particles, resin composition for three-dimensional modeling, and method for producing three-dimensional object using the same | |
Arrigo et al. | 10 Polymers Manufacturing for Additive | |
KR102473146B1 (en) | Composition for 3D Printing and Filament for 3D Printer | |
JP2010269587A (en) | Method for producing molded body and molded body | |
Arrigo et al. | Polymers for Additive Manufacturing | |
Clark et al. | Bredt et a |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
REG | Reference to a national code |
Ref country code: HK Ref legal event code: DE Ref document number: 1067905 Country of ref document: HK |
|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
CI01 | Publication of corrected invention patent application |
Correction item: Priority Correct: 09/854,220 20010511 US Number: 40 Volume: 26 |
|
CI03 | Correction of invention patent |
Correction item: Priority Correct: O9/854,220 20010511 US Number: 40 Page: The title page Volume: 26 |
|
ERR | Gazette correction |
Free format text: CORRECT: PRIORITY; FROM: NONE TO: 09/854,220;20010511;US |
|
REG | Reference to a national code |
Ref country code: HK Ref legal event code: GR Ref document number: 1067905 Country of ref document: HK |
|
CX01 | Expiry of patent term | ||
CX01 | Expiry of patent term |
Granted publication date: 20101006 |